View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00116U 26149.50819273 +.00000000 +00000-0 +74417-4 0 00005
2 00116 66.8099 296.5363 0082004 284.8492 74.3515 13.92328320 01
| Epoch (UTC): | 29 May 2026 12:11:47 |
| Eccentricity: | 0.0082004 |
| inclination: | 66.8099° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 296.5363° |
| argument of perigee: | 284.8492° |
| revolutions per day: | 13.92328320 |
| mean anomaly at epoch: | 74.3515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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